Rotary internal combustion engine with pilot subchamber

Patent metadata

Field	Value
Publication number	US-10697365-B2
Application number	US-201816168045-A
Country	US
Kind code	B2
Filing date	Oct 23, 2018
Priority date	Jul 28, 2011
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

A rotary engine having an insert in a peripheral wall of the stator body, the insert being made of a material having a greater heat resistance than that of the peripheral wall, having a subchamber defined therein and having an inner surface, the subchamber communicating with the cavity through at least one opening defined in the inner surface and having a shape forming a reduced cross-section adjacent the opening, a pilot fuel injector having a tip received in the subchamber, an ignition element having a tip received in the subchamber, and a main fuel injector extending through the stator body and having a tip communicating with the cavity at a location spaced apart from the insert. The subchamber has a volume corresponding to from 5% to 25% of a sum of the minimum volume and the volume of the subchamber. A method of injecting heavy fuel into a Wankel engine is also discussed.

First claim

The invention claimed is:

1. A rotary engine comprising:
a stator body;
a rotor body in sealing engagement with a wall of the stator body to define a plurality of working chambers in a cavity between the rotor body and the wall of the stator body, a volume of at least one of the plurality of working chambers varies between a minimum volume and a maximum volume, a displacement volume defined as the difference between the maximum volume and the minimum volume of one of the plurality of working chambers;
a pilot subchamber defined of a material having a greater heat resistance than that of the wall of the stator body, the pilot subchamber communicating with the cavity through at least one opening, the pilot subchamber having a volume corresponding to at least 0.5% and up to 3.5% of the displacement volume and/or corresponding to from 5% to 25% of a sum of the minimum volume and the volume of the subchamber;
a pilot fuel injector and an ignition element communicating with the pilot subchamber; and
a main fuel injector communicating with the cavity independently from the pilot subchamber.

2. The rotary engine defined in claim 1 , further comprising an insert in the wall of the stator body, the pilot subchamber being at least partly defined in the insert.

3. The rotary engine defined in claim 2 , wherein the insert has an inner surface bordering the cavity.

4. The rotary engine defined in claim 3 , wherein the at least one opening is defined in the inner surface of the insert and has a shape forming a reduced cross-section adjacent the opening.

5. The rotary engine defined in claim 2 , wherein the insert has an elongated body extending across a thickness of the wall of the stator body.

6. The rotary engine defined in claim 2 , wherein the insert has a flange at an outer end thereof, which is biased away from a shoulder defined in the wall of the stator body.

7. The rotary engine defined in claim 6 , wherein a spring between the flange and the shoulder biases the insert against a cover mounted to an outer surface of the wall of the stator body.

8. The rotary engine defined in claim 2 , wherein the insert has an inner surface which is continuous with an inner surface of the wall of the stator body to define the cavity.

9. The rotary engine defined in claim 2 , wherein the wall of the stator body defines a pilot injector hole in proximity of the insert for receiving the pilot fuel injector, and wherein the insert has an injector opening defined therethrough to provide communication between the pilot injector elongated hole and the subchamber.

10. The rotary engine defined in claim 9 , wherein the insert defines an ignition element elongated hole in communication with the subchamber, the ignition element being received in the ignition element elongated hole.

11. The rotary engine defined in claim 2 , wherein the insert includes an inner body portion and an outer body portion, and wherein the pilot subchamber is defined in the insert at a junction between the inner body portion and the outer body portion with the inner body portion defining the at least one opening for communication between the subchamber and the cavity.

12. The rotary engine defined in claim 11 , wherein the outer body portion defines an ignition element hole for receiving the ignition element.

13. The rotary engine defined in claim 1 , wherein the volume of the subchamber corresponds to from 0.625% to 1.25% of the displacement volume.

Assignees

• Pratt & Whitney Canada

Inventors

• Thomassin Jean
• Davenport Nigel
• Gekht Eugene

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F01C1/22

  of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member · CPC title

• F01C20/10

  characterised by changing the positions of the inlet or outlet openings with respect to the working chamber · CPC title

• F01C20/06

  specially adapted for stopping, starting, idling or no-load operation · CPC title

• F02B55/08 Primary

  Outer members for co-operation with rotary pistons; Casings · CPC title